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| 碟形飞行器复合控制方式研究 | |
| 引用本文： | 邬寅生,于德海,张友安,徐爱敏.碟形飞行器复合控制方式研究[J].海军航空工程学院学报,2009,24(5):551-555. |
| 作者姓名： | 邬寅生 于德海 张友安 徐爱敏 |
| 作者单位： | 1. 海军航空工程学院研究生管理大队,山东,烟台,264001 2. 海军航空工程学院训练部,山东,烟台,264001 3. 海军航空工程学院控制工程系,山东,烟台,264001 4. 烟台市人事局,山东,烟台,264000 |
| 基金项目： | 总装备部武器装备重点基金 |
| 摘 要： | 针对用两种方法控制的碟形飞行器，提出了三种不同的控制方式。按两执行机构之间的分配关系分为不分配、伪逆控制分配和比例控制分配。考虑执行机构动态，分别设计了三种控制方式下的变结构控制律，并研究了三种控制律下系统的跟踪性能。仿真结果表明比例控制分配法的控制效果最佳。 |
| 关 键 词： | 飞行器控制 复合控制 控制分配 变结构控制 |
Research on Composite Control Modes of Flying Saucer |
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| WU Yin-sheng,YU De-hai,ZHANG You-an and XU Ai-min.Research on Composite Control Modes of Flying Saucer[J].Journal of Naval Aeronautical Engineering Institute,2009,24(5):551-555. | |
| Authors: | WU Yin-sheng YU De-hai ZHANG You-an and XU Ai-min |
| Institution: | ( Naval Aeronautical and Astronautical University 1. Graduate Students＇ Brigade： 2. Department of Training： 3. Department of Control Engineering, Yantai Shandong 264001, China; 4. Bureau of Personnel, Yantai Shandong 264000, China) |
| Abstract: | Three control modes were presented to the flying saucer which controlled by thrust vectoring and mass. The relation between two actuators included no allocation, pseudoinverse control allocation and proportion control allocation. The actuator dynamics was considered. The variable structure control laws of different control modes were designed. The tracking performances of different control laws were investigated. Simulation results show that proportion control allocation has the best control effect. |
| Keywords: | control of aircraft composite control control allocation variable structure control |
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